民用飞机铰链式襟翼运动机构运动误差分析

Motion Tolerance Analysis for Flap LinkageArchitecture of Civil Aircraft

主要对民用飞机铰链式襟翼运动机构运动误差进行了分析。铰链式襟翼运动机构是目前国内外民用飞机主要采用的一种运动机构。采用极限误差累积的方法,详细分析了造成襟翼运动机构运动误差的各种原因,并对其造成的误差进行了分析。通过误差的分析,可以保证在满足飞机性能的同时,又很好地控制了飞机的成本。

Thisarticle is an analysis for motion tolerance for flap linkage architecture of civil aircraft. The flap linkage architecture is mostly used for flap of inside and outside of country. The article is detailed analysis all the reason caused the tolerance. From this, it can ensure that the flap motion architecture meet the aircraft performance requirement also well controlled the cost of the aircraft.